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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Principles of Flight > In a linear incompressible model of a swept-wing aeroplane at unchanged dynamic pressure, lift coefficient and configuration, ignore Mach effects and assume that the aerodynamic coefficients remain unchanged. As altitude and TAS increase, static lateral stability (1) and natural aerodynamic roll/yaw damping (2) will:

12 - ATPL Question Bank in English - In a linear incompressible model of a swept-wing aeroplane at unchanged dynamic pressure, lift coefficient and configuration, ignore Mach effects and assume that the aerodynamic coefficients remain unchanged. As altitude and TAS increase, static lateral stability (1) and natural aerodynamic roll/yaw damping (2) will:

Question 12 - Principles of Flight - ATPL - Airline Transport Pilot Licence

(1) increase (2) increase

(1) remain unchanged; (2) decrease.

(1) decrease (2) increase

(1) decrease (2) decrease

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